The influence of the loading path on the failure locus of a composite lamina subjected to transverse compression and out-of-plane shear is analyzed through computational micromechanics. This is carried out using the finite element simu-lation of a representative volume element of the micro structure, which takes into account explicitly fiber and matrix spatial distribution within the lamina. In addition, the actual failure mechanisms (plastic deformation of the matrix and interface decohesion) are included in the simulations through the corresponding constitutive models. Two different interface strength values were chosen to explore the limiting cases of composites with strong or weak interfaces. It was found that failure locus was independ...
Composite laminates can exhibit the nonlinear properties due to the fiber/matrix interface debonding...
ABSTRACT: A micromechanics-based constituent progressive damage model was proposed in this study to ...
In this paper, a new failure theory for laminated composite based on initiating failure mechanism is...
AbstractThe influence of the loading path on the failure locus of a composite lamina subjected to tr...
The influence of the loading path on the failure locus of a composite lamina subjected to transverse...
The influence of the loading path on the failure locus of a composite lamina subjected to transverse...
AbstractThe influence of the loading path on the failure locus of a composite lamina subjected to tr...
The failure locus a fiber-reinforced composite lamina, made up of 50 vol. % of carbon fibers embedde...
The failure locus a fiber-reinforced composite lamina, made up of 50 vol.% of carbon fibers embedded...
AbstractA method for determining the in situ strength of fiber-reinforced laminas for three types of...
Fibre reinforced composites exhibit a gradual damage accumulation to failure, with a multitude of hi...
ABSTRACT: The micromechanics of failure was developed to predict the failure of continuous fiber rei...
The effect of porosity on the transverse mechanical properties of unidirectional fiber-reinforced co...
The potential of computational micromechanics to predict the failure locus of a unidirectional C/PEE...
peer-reviewedFibre reinforced composites exhibit a gradual damage accumulation to failure, with a m...
Composite laminates can exhibit the nonlinear properties due to the fiber/matrix interface debonding...
ABSTRACT: A micromechanics-based constituent progressive damage model was proposed in this study to ...
In this paper, a new failure theory for laminated composite based on initiating failure mechanism is...
AbstractThe influence of the loading path on the failure locus of a composite lamina subjected to tr...
The influence of the loading path on the failure locus of a composite lamina subjected to transverse...
The influence of the loading path on the failure locus of a composite lamina subjected to transverse...
AbstractThe influence of the loading path on the failure locus of a composite lamina subjected to tr...
The failure locus a fiber-reinforced composite lamina, made up of 50 vol. % of carbon fibers embedde...
The failure locus a fiber-reinforced composite lamina, made up of 50 vol.% of carbon fibers embedded...
AbstractA method for determining the in situ strength of fiber-reinforced laminas for three types of...
Fibre reinforced composites exhibit a gradual damage accumulation to failure, with a multitude of hi...
ABSTRACT: The micromechanics of failure was developed to predict the failure of continuous fiber rei...
The effect of porosity on the transverse mechanical properties of unidirectional fiber-reinforced co...
The potential of computational micromechanics to predict the failure locus of a unidirectional C/PEE...
peer-reviewedFibre reinforced composites exhibit a gradual damage accumulation to failure, with a m...
Composite laminates can exhibit the nonlinear properties due to the fiber/matrix interface debonding...
ABSTRACT: A micromechanics-based constituent progressive damage model was proposed in this study to ...
In this paper, a new failure theory for laminated composite based on initiating failure mechanism is...